CN107985567A - It is a kind of based on the nose wheel steering mechanism for having man-machine unmanned repacking - Google Patents
It is a kind of based on the nose wheel steering mechanism for having man-machine unmanned repacking Download PDFInfo
- Publication number
- CN107985567A CN107985567A CN201711455455.2A CN201711455455A CN107985567A CN 107985567 A CN107985567 A CN 107985567A CN 201711455455 A CN201711455455 A CN 201711455455A CN 107985567 A CN107985567 A CN 107985567A
- Authority
- CN
- China
- Prior art keywords
- nose wheel
- man
- steering engine
- wheel steering
- steering mechanism
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 230000007246 mechanism Effects 0.000 title claims abstract description 62
- 238000012857 repacking Methods 0.000 title claims abstract description 51
- 238000013461 design Methods 0.000 claims abstract description 7
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 claims description 6
- 210000005069 ears Anatomy 0.000 claims description 3
- 238000003780 insertion Methods 0.000 claims description 3
- 230000037431 insertion Effects 0.000 claims description 3
- 238000003466 welding Methods 0.000 claims 1
- 238000009434 installation Methods 0.000 abstract description 4
- 238000005516 engineering process Methods 0.000 description 4
- 230000009471 action Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 2
- 230000008901 benefit Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000008859 change Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000012937 correction Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/50—Steerable undercarriages; Shimmy-damping
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Steering-Linkage Mechanisms And Four-Wheel Steering (AREA)
Abstract
Present disclose provides a kind of based on the nose wheel steering mechanism for having man-machine unmanned repacking, including servo straight line steering engine, steering engine stent, push-pull rod, front band and lower catch hoop.Servo straight line steering engine tail end is connected with steering engine stent, and stent is fixed on aircraft main force support structure.Steering engine front end output shaft is connected with push-pull rod auricle, and the push-pull rod other end is fixed with lower catch hoop sleeve connection.Patch rubber pad, is fixed around rudder of aircraft pedal column obvolvent in upper lower catch hoop, and prevents opposite slide through clip and column with stay bolt.The nose wheel steering mechanism structure of the present invention is simple, reliable operation and versatile, there is the design and installation of the nose wheel steering mechanism of man-machine unmanned repacking suitable for the overwhelming majority.
Description
Technical field
The disclosure, which belongs to, man-machine unmanned retrofit technology field, and in particular to a kind of based on there is man-machine unmanned repacking
Nose wheel steering mechanism.
Background technology
With the development of unmanned plane industry, risk can be reduced, shorten and grind by having man-machine unmanned repacking to be increasingly becoming one kind
Cycle processed, easy and effective and the huge market demand technological means.The foresteerage gear of undercarriage is for aircraft floor
Traveling is turned, landing slides the wide-angle correction run and plays an important role, its unmanned repacking is also in whole repacking work
One difficult point.
The content of the invention
(1) technical problems to be solved
Present disclose provides a kind of based on the nose wheel steering mechanism for having man-machine unmanned repacking, at least partly to solve
Technical problem set forth above.
(2) technical solution
Present disclose provides a kind of based on the nose wheel steering mechanism for having man-machine unmanned repacking, including：Servo straight line
Steering engine 110, it includes fuselage 111 and output shaft 112, and 111 afterbody of fuselage has fixed auricle, and there is connection in 112 front end of output shaft
Auricle；Steering engine stent 120, is connected by bolt with the fixation auricle of fuselage 111；Push-pull rod 130, L-shaped, its one end passes through spiral shell
Bolt is connected with the attachment lug of 112 front end of output shaft；Lower catch hoop 140, including lower catch hoop sleeve and semicircle lower catch hoop, push-pull rod
In 130 other end insertion lower catch hoop sleeve；And front band 150, including semicircle front band, it passes through spiral shell with semicircle lower catch hoop
Tether and connect.
In some embodiments of the present disclosure, fuselage 111 is fixed for front and rear two point form, it is connected to winged by electric interfaces
Row control computer；Output shaft 112 is extending or shrinks.
In some embodiments of the present disclosure, steering engine stent 120 is door shape stent, it is by the front foot of steering engine stent with after
Foot is fixed on aircraft main force support structure.
In some embodiments of the present disclosure, door shape stent is by the way that steering engine frame height is connected needed for start to whole mechanism
Highly meet steering angle design requirement.
In some embodiments of the present disclosure, one end of push-pull rod 130 is connected with lower catch hoop sleeve by being interference fitted, and is protected
130 monaural of push-pull rod, servo straight line steering engine 110 and the connection of steering engine stent 120 are demonstrate,proved on same axis and from side force, sleeve
Junction extends radially through fixation with axis pin.
In some embodiments of the present disclosure, 120 monaural of steering engine stent in 130 monaural of push-pull rod with being embedded with centripetal joint
Bearing, bolt are attached through bearing with 110 ears piece of servo straight line steering engine, ensure servo straight line steering engine 110 and push-pull rod
130 can rotate around tie point.
In some embodiments of the present disclosure, rubber pad is posted in semicircle lower catch hoop and semicircle front band；Semicircle lower catch hoop
It is bolted with semicircle front band, around 200 obvolvent of rudder of aircraft pedal column.
In some embodiments of the present disclosure, semicircle lower catch hoop and semicircle front band obvolvent position are along pedals column
About 200 is adjustable, is adjusted to after meeting the requirement of front-wheel steer angle, is fixed by stay bolt through clip and column.
In some embodiments of the present disclosure, nose wheel steering mechanism 100 by front band 150 and lower catch hoop 140 with
Pedals column 200 is connected, and pedals column 200 is welded on transverse tube at the top of Yuan Ji pedals steering mechanism
On, top transverse tube is bolt-connected to aircraft fixed ear on piece and is rotated around auricle, and top transverse tube welds a cantilever and passes through spiral shell
Bolt is connected composition linkage with push-pull rod 130, and 130 other end of push-pull rod is connected by bolt with the top of steering arm 300；
Servo straight line steering engine 110 receives steering order of the flight-control computer to rudder control device, and instruction is turned right, and output shaft 112 is extended, pushed away
Dynamic front band 150 and lower catch hoop 140 and pedals column 200 forward, pedals column 200 by top transverse tube around
Aircraft fixes auricle and does movement in a curve, drives linkage driving nose wheel steering bar 300 to complete to turn right；Instruction is turned left, defeated
Shaft 112 is shunk, and pulls the front band 150 and the lower catch hoop 140 and the pedals column 200 backward, is driven
Linkage driving nose wheel steering bar 300 is completed.
In some embodiments of the present disclosure, whole mechanism connection, which is in, is not loaded with state.
(3) beneficial effect
It can be seen from the above technical proposal that the disclosure based on the nose wheel steering mechanism for having man-machine unmanned repacking
At least have the advantages that one of them：
(1) based on the nose wheel steering mechanism structure that has man-machine unmanned repacking is simple, light-weight, reliable operation；
(2) it is versatile based on the nose wheel steering mechanism structure for having man-machine unmanned repacking, suitable for the overwhelming majority
There is the design and installation of the nose wheel steering mechanism of man-machine unmanned repacking.
Brief description of the drawings
Fig. 1 is the nose wheel steering mechanism isometric view of unmanned repacking in the embodiment of the present disclosure.
Fig. 2 a are servo straight line steering engine front view in the nose wheel steering mechanism of unmanned repacking in the embodiment of the present disclosure.
Fig. 2 b are servo straight line steering engine top view in the nose wheel steering mechanism of unmanned repacking in the embodiment of the present disclosure.
Fig. 3 is the nose wheel steering mechanism centered rudder machine support front view of unmanned repacking in the embodiment of the present disclosure.
Fig. 4 a are push-pull rod front view in the nose wheel steering mechanism of unmanned repacking in the embodiment of the present disclosure.
Fig. 4 b are push-pull rod side view in the nose wheel steering mechanism of unmanned repacking in the embodiment of the present disclosure.
Fig. 5 a are lower catch hoop front view in the nose wheel steering mechanism of unmanned repacking in the embodiment of the present disclosure.
Fig. 5 b are lower catch hoop side view in the nose wheel steering mechanism of unmanned repacking in the embodiment of the present disclosure.
Fig. 6 a are front band front view in the nose wheel steering mechanism of unmanned repacking in the embodiment of the present disclosure.
Fig. 6 b are front band side view in the nose wheel steering mechanism of unmanned repacking in the embodiment of the present disclosure.
Fig. 7 is that the unmanned repacking for having man-machine front-wheel steer in the embodiment of the present disclosure manipulates schematic diagram.
【Embodiment of the present disclosure main element symbol description in attached drawing】
100- nose wheel steerings mechanism；
110- servo straight line steering engines；
111- fuselages；112- output shafts；
120- steering engine stents；130- push-pull rods；
140- lower catch hoops；150- front bands；
200- pedals columns；
300- steering arms.
Embodiment
Present disclose provides a kind of based on the nose wheel steering mechanism for having man-machine unmanned repacking, including servo straight line rudder
Machine, steering engine stent, push-pull rod, front band and lower catch hoop.Servo straight line steering engine tail end is connected with steering engine stent, and stent is fixed on
On aircraft main force support structure.Steering engine front end output shaft is connected with push-pull rod auricle, the push-pull rod other end and lower catch hoop sleeve connection
It is fixed.Patch rubber pad, is fixed around rudder of aircraft pedal column obvolvent in upper lower catch hoop, and through clip and is stood with stay bolt
Column prevents opposite slide.The nose wheel steering mechanism structure of the present invention is simple, reliable operation and versatile, suitable for big absolutely
There is the design and installation of the nose wheel steering mechanism of man-machine unmanned repacking in part.
For the purpose, technical scheme and advantage of the disclosure are more clearly understood, below in conjunction with specific embodiment, and reference
Attached drawing, is further described the disclosure.
Disclosure some embodiments will be done with reference to appended attached drawing in rear and more comprehensively describe to property, some of but not complete
The embodiment in portion will be illustrated.In fact, the various embodiments of the disclosure can be realized in many different forms, and should not be construed
To be limited to this several illustrated embodiment；Relatively, there is provided these embodiments cause the disclosure to meet applicable legal requirement.
In an exemplary embodiment of the disclosure, there is provided a kind of based on the front-wheel steer for having man-machine unmanned repacking
Operating mechanism.
Fig. 1 is the nose wheel steering mechanism isometric view of unmanned repacking in the embodiment of the present disclosure.As shown in Figure 1,
The disclosure is included based on the nose wheel steering mechanism for having man-machine unmanned repacking：
Servo straight line steering engine 110, including
Fuselage 111, its afterbody have fixed auricle；And
There are attachment lug in output shaft 112, its front end；
Steering engine stent 120, is connected by bolt with the fixation auricle of fuselage 111；
Push-pull rod 130, L-shaped, its one end is connected by bolt with the attachment lug of 112 front end of output shaft；
Lower catch hoop 140, including lower catch hoop sleeve and semicircle lower catch hoop, the other end insertion lower catch hoop sleeve of push-pull rod 130
It is interior；And
Front band 150, including semicircle front band, it is bolted with semicircle lower catch hoop.
Portion is formed based on each of nose wheel steering mechanism by man-machine unmanned repacking to the present embodiment individually below
Divide and be described in detail.
Fig. 2 a, 2b are servo straight line steering engine front view and top view in the nose wheel steering mechanism of unmanned repacking.Such as
Fig. 2 a, shown in 2b, servo straight line steering engine 110 includes：
Fuselage 111, it is fixed for front and rear two point form, it is connected to flight-control computer by electric interfaces；And
Output shaft 112, it can extend or shrink.
Fig. 3 is the front view of the nose wheel steering mechanism centered rudder machine support of unmanned repacking.As shown in figure 3, steering engine branch
Frame 120 is door shape stent, is fixed on by the front foot of steering engine stent and the rear foot on aircraft main force support structure；Door shape stent can
Steering engine frame is high to whole mechanism connection start desired height so as to meet steering angle design requirement, and be avoided that and set with remaining
Standby interference.
Fig. 4 a, 4b are push-pull rod front view and side view in the nose wheel steering mechanism of unmanned repacking.Such as Fig. 4 a, 4b
Shown, push-pull rod 130, its one end is connected with lower catch hoop sleeve by being interference fitted, and ensures 130 monaural of push-pull rod, servo straight line
Steering engine 110 and the connection of steering engine stent 120 are extended radially through solid on the same axis and from side force at sleeve connection with axis pin
It is fixed.
Fig. 5 a, 5b are lower catch hoop front view and side view in the nose wheel steering mechanism of unmanned repacking.Such as Fig. 5 a, 5b
It is shown, lower catch hoop 140, including
Lower catch hoop sleeve；And
Semicircle lower catch hoop, inside posts rubber pad.
Fig. 6 a, 6b are front band front view and side view in the nose wheel steering mechanism of unmanned repacking.Such as Fig. 6 a, 6b
It is shown, front band 150, including
Semicircle front band, inside posts rubber pad, semicircle front band is bolted with semicircle lower catch hoop, around aircraft side
To 200 obvolvent of rudder pedal column, obvolvent position along pedal column about 200 it is adjustable, examination to be adjusted action meets front wheel steering angle
After degree requires, being fixed with stay bolt through clip and column prevents relative motion.
Fig. 7 is that the unmanned repacking for having man-machine front-wheel steer in the embodiment of the present disclosure manipulates schematic diagram.As shown in fig. 7, make
When dynamic, steering engine output shaft 112 is extended or shunk, and is driven front end push-pull rod 130 and clip movement, is turned by former machine pedals
Torque is transmitted to mechanism, driving nose wheel steering bar 300 turns to.
For example：
(1) servo straight line steering engine 110 receives steering order of the flight-control computer to rudder control device, and instruction is turned right, output
Axis 112 extends, and promotes clip 140,150 and pedal column 200 forward, pedal column 200 is consolidated by top transverse tube around inverted triangle
Determine auricle and do movement in a curve, drive linkage driving nose wheel steering bar 300 to complete to turn right；
(2) servo straight line steering engine 110 receives steering order of the flight-control computer to rudder control device, and instruction is turned left, output
Axis 112 is shunk, and pulls clip 140,150 and pedal column 200 backward, and pedal column 200 drives rotation before linkage driving
Complete to control stick 300.
It should be noted that 120 monaural of steering engine stent in 130 monaural of push-pull rod with being embedded with plain radial bearing, bolt
It is attached through bearing and 110 ears piece of servo straight line steering engine, ensures that servo straight line steering engine 110 can be around even with push-pull rod 130
Contact rotates.
It should be noted that clip obvolvent position is along adjustable above and below pedal column, rotation before meeting by adjusting examination action
To after angle requirement, then fixed with stay bolt through clip and column and prevent relative motion.
It should be noted that whole mechanism connection is in and is not loaded with state.
So far, one embodiment of the disclosure is a kind of based on the nose wheel steering mechanism introduction for having man-machine unmanned repacking
Finish.
So far, attached drawing is had been combined the embodiment of the present disclosure is described in detail.According to above description, art technology
Personnel should have clear understanding to the present invention based on the nose wheel steering mechanism for having man-machine unmanned repacking.
It should be noted that in attached drawing or specification text, the implementation that does not illustrate or describe is affiliated technology
Form known to a person of ordinary skill in the art, is not described in detail in field.In addition, the above-mentioned definition to each element and method is simultaneously
Various concrete structures, shape or the mode mentioned in embodiment are not limited only to, those of ordinary skill in the art can carry out letter to it
Singly change or replace.
In conclusion present disclose provides a kind of based on the nose wheel steering mechanism for having man-machine unmanned repacking, including
Servo straight line steering engine, steering engine stent, push-pull rod, front band and lower catch hoop.Servo straight line steering engine tail end is connected with steering engine stent,
Stent is fixed on aircraft main force support structure.Steering engine front end output shaft is connected with push-pull rod auricle, the push-pull rod other end and lower card
Ferrule sleeve connection is fixed.Patch rubber pad, is fixed, and passed through with stay bolt around rudder of aircraft pedal column obvolvent in upper lower catch hoop
Wearing clip and column prevents opposite slide.The nose wheel steering mechanism structure of the present invention is simple, reliable operation and versatile,
There is the design and installation of the nose wheel steering mechanism of man-machine unmanned repacking suitable for the overwhelming majority.
It should also be noted that, the direction term mentioned in embodiment, for example, " on ", " under ", "front", "rear", " left side ",
" right side " etc., is only the direction of refer to the attached drawing, is not used for limiting the protection domain of the disclosure.Through attached drawing, identical element by
Same or like reference numeral represents.When understanding of this disclosure may be caused to cause to obscure, conventional structure will be omitted
Or construction.
And the shape and size of each component do not reflect actual size and ratio in figure, and only illustrate the embodiment of the present disclosure
Content.In addition, in the claims, any reference symbol between bracket should not be configured to the limit to claim
System.
Furthermore word "comprising" does not exclude the presence of element or step not listed in the claims.Before element
Word "a" or "an" does not exclude the presence of multiple such elements.
Similarly, it will be appreciated that in order to simplify the disclosure and help to understand one or more of each open aspect,
Above in the description to the exemplary embodiment of the disclosure, each feature of the disclosure is grouped together into single implementation sometimes
In example, figure or descriptions thereof.However, the method for the disclosure should be construed to reflect following intention：I.e. required guarantor
The disclosure of shield requires features more more than the feature being expressly recited in each claim.It is more precisely, such as following
Claims reflect as, open aspect is all features less than single embodiment disclosed above.Therefore,
Thus the claims for following embodiment are expressly incorporated in the embodiment, wherein each claim is in itself
Separate embodiments all as the disclosure.
Particular embodiments described above, has carried out further in detail the purpose, technical solution and beneficial effect of the disclosure
Describe in detail bright, it should be understood that the foregoing is merely the specific embodiment of the disclosure, be not limited to the disclosure, it is all
Within the spirit and principle of the disclosure, any modification, equivalent substitution, improvement and etc. done should be included in the guarantor of the disclosure
Within the scope of shield.
Claims (10)
1. it is a kind of based on the nose wheel steering mechanism for having man-machine unmanned repacking, including：
Servo straight line steering engine (110), including
Fuselage (111), its afterbody have fixed auricle；And
There are attachment lug in output shaft (112), its front end；
Steering engine stent (120), is connected by bolt with the fixation auricle of the fuselage (111)；
Push-pull rod (130), L-shaped, its one end is connected by bolt with the attachment lug of the output shaft (112) front end；
Lower catch hoop (140), including lower catch hoop sleeve and semicircle lower catch hoop, the push-pull rod (130) the other end insertion it is described under
In clip sleeve；And
Front band (150), including semicircle front band, it is bolted with the semicircle lower catch hoop.
2. it is according to claim 1 based on the nose wheel steering mechanism for having man-machine unmanned repacking, wherein,
The fuselage (111) is fixed for front and rear two point form, it is connected to flight-control computer by electric interfaces；
The output shaft (112) is extending or shrinks.
3. it is according to claim 1 based on the nose wheel steering mechanism for having man-machine unmanned repacking, wherein,
The steering engine stent (120) is door shape stent, it is fixed on aircraft primary load bearing knot by the front foot of steering engine stent and the rear foot
On structure.
4. it is according to claim 3 based on the nose wheel steering mechanism for having man-machine unmanned repacking, wherein,
The door shape stent meets that steering angle designs by the way that steering engine frame height to whole mechanism is connected start desired height
It is required that.
5. it is according to claim 1 based on the nose wheel steering mechanism for having man-machine unmanned repacking, wherein,
One end of the push-pull rod (130) is connected with the lower catch hoop sleeve by being interference fitted, and ensures the push-pull rod (130)
Monaural, the servo straight line steering engine (110) and the steering engine stent (120) connection are on same axis and from side force, set
Cylinder junction extends radially through fixation with axis pin.
6. it is according to claim 1 based on the nose wheel steering mechanism for having man-machine unmanned repacking, wherein,
For steering engine stent (120) monaural with being embedded with plain radial bearing in the push-pull rod (130) monaural, bolt passes through axis
Hold and be attached with servo straight line steering engine (110) the ears piece, ensure servo straight line steering engine (110) and the push-pull rod
(130) can be rotated around tie point.
7. it is according to claim 1 based on the nose wheel steering mechanism for having man-machine unmanned repacking, wherein,
Rubber pad is posted in the semicircle lower catch hoop and the semicircle front band；
The semicircle lower catch hoop is bolted with the semicircle front band, is embraced around rudder of aircraft pedal column (200)
Close.
8. it is according to claim 7 based on the nose wheel steering mechanism for having man-machine unmanned repacking, wherein,
The semicircle lower catch hoop is adjustable up and down along the pedals column (200) with the semicircle front band obvolvent position,
It is adjusted to after meeting the requirement of front-wheel steer angle, is fixed by stay bolt through clip and column.
9. it is according to claim 1 based on the nose wheel steering mechanism for having man-machine unmanned repacking, wherein,
The nose wheel steering mechanism (100) passes through the front band (150) and the lower catch hoop (140) and the rudder
Pedal column (200) is connected, and the pedals column (200) is welded on transverse tube at the top of Yuan Ji pedals steering mechanism
On, the top transverse tube is bolt-connected to aircraft fixed ear on piece and is rotated around auricle, and the top transverse tube welding one is outstanding
Arm is connected composition linkage by bolt with the push-pull rod (130), and push-pull rod (130) other end passes through bolt and institute
State connection at the top of steering arm (300)；
Servo straight line steering engine (110) receives steering order of the flight-control computer to rudder control device, and instruction is turned right, output shaft
(112) extend, promote the front band (150) and the lower catch hoop (140) and the pedals column (200) forward,
The pedals column (200) fixes auricle around the aircraft by the top transverse tube and does movement in a curve, drives connecting rod
Mechanism driving nose wheel steering bar (300) is completed to turn right；Instruction is turned left, and output shaft (112) is shunk, and pulls the front band
(150) and the lower catch hoop (140) and the pedals column (200) backward, drive linkage driving front-wheel steer
Control stick (300) is completed.
10. it is according to claim 1 based on the nose wheel steering mechanism for having man-machine unmanned repacking, wherein,
Whole mechanism connection, which is in, is not loaded with state.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711455455.2A CN107985567B (en) | 2017-12-27 | 2017-12-27 | Front wheel steering control mechanism based on unmanned modification of man-machine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711455455.2A CN107985567B (en) | 2017-12-27 | 2017-12-27 | Front wheel steering control mechanism based on unmanned modification of man-machine |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN107985567A true CN107985567A (en) | 2018-05-04 |
| CN107985567B CN107985567B (en) | 2024-03-12 |
Family
ID=62043193
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711455455.2A Active CN107985567B (en) | 2017-12-27 | 2017-12-27 | Front wheel steering control mechanism based on unmanned modification of man-machine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107985567B (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110271689A (en) * | 2019-06-03 | 2019-09-24 | 西安飞机工业（集团）有限责任公司 | A kind of electronic detection device of aircraft nose wheel turning |
| CN110466747A (en) * | 2019-09-18 | 2019-11-19 | 朗星无人机***有限公司 | A kind of Large freight unmanned plane nose wheel steering mechanism |
| CN110641685A (en) * | 2019-11-11 | 2020-01-03 | 中国科学院工程热物理研究所 | Front wheel steering control mechanism |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20130137336A1 (en) * | 2010-08-13 | 2013-05-30 | Kanghan Ni | Linkage device for remote control model helicopter with coaxial and counter rotating double-propeller |
| CN203094436U (en) * | 2012-12-25 | 2013-07-31 | 天津三爻航空航天科技发展有限公司 | Tail-wheel steering apparatus of fixed wing aircraft |
| CN104859848A (en) * | 2015-04-30 | 2015-08-26 | 中国科学院长春光学精密机械与物理研究所 | Front wheel steering mechanism suitable for unmanned aerial vehicle |
| CN208233351U (en) * | 2017-12-27 | 2018-12-14 | 中国科学院工程热物理研究所 | It is a kind of based on the nose wheel steering mechanism for having man-machine unmanned repacking |
-
2017
- 2017-12-27 CN CN201711455455.2A patent/CN107985567B/en active Active
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20130137336A1 (en) * | 2010-08-13 | 2013-05-30 | Kanghan Ni | Linkage device for remote control model helicopter with coaxial and counter rotating double-propeller |
| CN203094436U (en) * | 2012-12-25 | 2013-07-31 | 天津三爻航空航天科技发展有限公司 | Tail-wheel steering apparatus of fixed wing aircraft |
| CN104859848A (en) * | 2015-04-30 | 2015-08-26 | 中国科学院长春光学精密机械与物理研究所 | Front wheel steering mechanism suitable for unmanned aerial vehicle |
| CN208233351U (en) * | 2017-12-27 | 2018-12-14 | 中国科学院工程热物理研究所 | It is a kind of based on the nose wheel steering mechanism for having man-machine unmanned repacking |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110271689A (en) * | 2019-06-03 | 2019-09-24 | 西安飞机工业（集团）有限责任公司 | A kind of electronic detection device of aircraft nose wheel turning |
| CN110466747A (en) * | 2019-09-18 | 2019-11-19 | 朗星无人机***有限公司 | A kind of Large freight unmanned plane nose wheel steering mechanism |
| CN110641685A (en) * | 2019-11-11 | 2020-01-03 | 中国科学院工程热物理研究所 | Front wheel steering control mechanism |
Also Published As
| Publication number | Publication date |
|---|---|
| CN107985567B (en) | 2024-03-12 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN208233351U (en) | It is a kind of based on the nose wheel steering mechanism for having man-machine unmanned repacking | |
| CN107985567A (en) | It is a kind of based on the nose wheel steering mechanism for having man-machine unmanned repacking | |
| EP2794384B1 (en) | Dual steering system for a vehicle | |
| DE102014225599B4 (en) | Wishbone arrangement | |
| KR20170066567A (en) | A directional control system and method for a hybrid air and ground transportation vehicle | |
| CN206812741U (en) | The double yoke suspensions of electric automobile | |
| US20160176493A1 (en) | Rudder | |
| AU701123B2 (en) | Rack and pinion steering system for four wheel drive vehicle | |
| EP2025580B1 (en) | Steering group of the wheels of an axle of a vehicle | |
| EP3162607A1 (en) | Unsprung power supply apparatus for in-wheel motor vehicle | |
| CN106081102A (en) | A kind of unmanned plane and bar thick stick formula tail-rotor distance changing mechanism thereof | |
| CN100408362C (en) | Independent suspension for vehicle | |
| US8893846B2 (en) | Power assisted steering assembly | |
| KR20170125062A (en) | Independent wheel suspension system with large steering angle | |
| EP2165862B1 (en) | Device for adjusting a wheel of a wheel suspension | |
| GB2521454A (en) | Support casing for a differential gear of an axle and track rod assembly | |
| US20180178901A1 (en) | Wing for an aircraft | |
| CN105835947A (en) | Multi-axis synchronous steering system for automobile underpan | |
| CN205738066U (en) | One turns to undercarriage to control to subtract oscillator system | |
| DE102017216983A1 (en) | independent suspension | |
| US9174727B2 (en) | Landing gear steering using eccentric bearings | |
| CN205087009U (en) | Steering system | |
| CN108216599A (en) | A kind of big nose wheel steering mechanism for manipulating angle of Double-linkage | |
| CN105905159A (en) | Three-section tie rod steering linkage rod system | |
| CN205998111U (en) | A kind of dirigible abnormity layout empennage operating mechanism |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant |